Nonlinear Adaptive Feedback Control for Spacecraft Proximity Formation Flying

Tao Xi; Jian Cheng Li; Wei Quan Pan

doi:10.4028/www.scientific.net/AMM.376.446

Paper Titles

Comparison of Bending Stress of a Helical Gear for Different Materials and Modules Using AGMA Standards in FEA
p.423

Simulation of MEMS Cantilever Biosensor and Analysis of Readout Methods for Tuberculosis Detection
p.428

Research on Image Binding Mechanism Based on Kinect Skeletal Tracking in Virtual Fitting System
p.437

Fault Diagnosis Method of Gearbox Based on Local Mean Decomposition
p.441

Nonlinear Adaptive Feedback Control for Spacecraft Proximity Formation Flying
p.446

Signal Detection Technology for Low Voltage Arc Fault Circuit Interrupter Using FPGA
p.451

Dynamic Targets Detection for Robotic Applications Using Panoramic Camera Based on Optical Flow
p.455

Distribution and Potential Risk of Copper in Surface Sediments of Anping Harbor, Taiwan
p.463

Hazard Identification & Risk Assesment in New Chassis Assembly Line
p.468

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 376Nonlinear Adaptive Feedback Control for Spacecraft...

Nonlinear Adaptive Feedback Control for Spacecraft Proximity Formation Flying

Abstract:

Spacecraft proximity formation flying is essential for future autonomous space mission such as autonomous rendezvous and docking and assembly of space system on-orbit. In order to improve the autonomy of relative motion control between two spacecrafts and concerning the effect of perturbation by bounded uncertain disturbance, a novel nonlinear adaptive feedback controller is developed based on sliding mode control law to maintain the desired reference trajectory as precisely as possible. The simulation results demonstrate the control scheme can effectively carry out the relative motion maintenance and have better asymptotically stability.

You might also be interested in these eBooks

Materials and Diverse Technologies in Industry and Manufacture

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 376)

Pages:

446-450

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.376.446

Citation:

Cite this paper

Online since:

August 2013

Authors:

Tao Xi, Jian Cheng Li, Wei Quan Pan

Keywords:

Formation Flying, Nonlinear Feedback Control, Sliding Model Control Law, Spacecraft

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] P. K. C. Wang and F. Y. Hadaegh. Coordination and control of multiple micro-spacecraft moving in formation. Journal of the Astronautical Sciences, 44(3): 315–355, (1996).

Google Scholar

[2] J. Lawton R. W. Beard and F. Y. Hadaegh. A coordination architecture for spacecraft formation control. IEEE Transactions on Control Systems Technology, 9(6): 777–790, (2001).

DOI: 10.1109/87.960341

Google Scholar

[3] W. Ren and R. W. Beard. Virtual structure based spacecraft formation control with formation feedback. In Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, p.1–8, (2002).

DOI: 10.2514/6.2002-4963

Google Scholar

[4] Hughes, S. P. and Mailhe, L. M., A Preliminary Formation Flying Orbit Dynamics Analysis for Leonardo-BRDF, " Flight Mechanics Symposium, NASA Goddard Space Flight Center, Greenbelt, MD, (2001).

DOI: 10.1109/aero.2001.931237

Google Scholar

[5] Schaub, H. and Alfriend, K. T., Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements, Journal of Guidance, Control, and Dynamics, 24(4): 739-745, (2001).

DOI: 10.2514/2.4774

Google Scholar

[6] L.S. Breger, Model Predictive Control for Formation Flying Spacecraft, S.M. Thesis, Massachusetts Institute of Technology, Dept. Aeronautics and Astronautics, June (2004).

Google Scholar

[7] Clohessy, W. H. and Wiltshire, R. S. Terminal Guidance System for Satellite Rendezvous, Journal of the Aerospace Sciences, 27: 653-658. (1960).

DOI: 10.2514/8.8704

Google Scholar

[8] Gim, D. -W. and Alfriend, K. T., State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit, Journal of Guidance, Control, and Dynamics, 26(6): 956–971, (2003).

DOI: 10.2514/2.6924

Google Scholar

[9] Pluym, J. P. and Damaren, C. J., Dynamics and Control of Spacecraft Formation Flying: Reference Orbit Selection and Feedback Control, Proc. 13th Canadian Astronautics Conference (ASTRO 2006), Montreal, Quebec, April 25-27, (2006).

Google Scholar

[10] Howard D Curtis, Orbital. Mechanics. for. Engineering. Students, Elsevier, June (2005).

Google Scholar